SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment
The first launch of the SHarp Edge Flight EXperiment (SHEFEX) was from Andøya Rocket Range (ARR) Norway, in October 2005. Its purpose was to investigate the aerodynamic behaviour and thermal problems of an unconventional shape for re-entry vehicles comprising multi-facetted surfaces with sharp edges...
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ftdlr:oai:elib.dlr.de:81994 2024-05-19T07:28:25+00:00 SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment Turner, John Hörschgen, Marcus Jung, Wolfgang Turner, Peter 2007 application/pdf https://elib.dlr.de/81994/ https://elib.dlr.de/81994/1/Visby-Turner-Report-SHEFEX_2.pdf de ger https://elib.dlr.de/81994/1/Visby-Turner-Report-SHEFEX_2.pdf Turner, John und Hörschgen, Marcus und Jung, Wolfgang und Turner, Peter (2007) SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment. In: Symposium Proceedings. 18th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2007-06-03 - 2007-06-07, Visby, Schweden. Mobile Raketenbasis Konferenzbeitrag NonPeerReviewed 2007 ftdlr 2024-04-25T00:26:10Z The first launch of the SHarp Edge Flight EXperiment (SHEFEX) was from Andøya Rocket Range (ARR) Norway, in October 2005. Its purpose was to investigate the aerodynamic behaviour and thermal problems of an unconventional shape for re-entry vehicles comprising multi-facetted surfaces with sharp edges and an asymmetric form and to provide a correlation of numerical predictions with the flight results for velocities up to the order of Mach 7. The success of the first mission has led to the approval of the SHEFEX 2 project which will involve a facetted but symmetrical fore body with a canard control system to obtain further data on the aerodynamic and thermal effects at hypersonic velocities. The canard system should provide control in all axes and predefined angles of attack of up to +/-5 degrees during the re-entry phase. The Mobile Rocket Base (MORABA) of the German Aerospace Centre (DLR) is again responsible for the vehicle, payload, service systems and test flight of the SHEFEX 2 experiment on a two-stage, solid propellant, sounding rocket. Conference Object Andøya German Aerospace Center: elib - DLR electronic library |
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German Aerospace Center: elib - DLR electronic library |
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German |
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Mobile Raketenbasis |
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Mobile Raketenbasis Turner, John Hörschgen, Marcus Jung, Wolfgang Turner, Peter SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
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Mobile Raketenbasis |
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The first launch of the SHarp Edge Flight EXperiment (SHEFEX) was from Andøya Rocket Range (ARR) Norway, in October 2005. Its purpose was to investigate the aerodynamic behaviour and thermal problems of an unconventional shape for re-entry vehicles comprising multi-facetted surfaces with sharp edges and an asymmetric form and to provide a correlation of numerical predictions with the flight results for velocities up to the order of Mach 7. The success of the first mission has led to the approval of the SHEFEX 2 project which will involve a facetted but symmetrical fore body with a canard control system to obtain further data on the aerodynamic and thermal effects at hypersonic velocities. The canard system should provide control in all axes and predefined angles of attack of up to +/-5 degrees during the re-entry phase. The Mobile Rocket Base (MORABA) of the German Aerospace Centre (DLR) is again responsible for the vehicle, payload, service systems and test flight of the SHEFEX 2 experiment on a two-stage, solid propellant, sounding rocket. |
format |
Conference Object |
author |
Turner, John Hörschgen, Marcus Jung, Wolfgang Turner, Peter |
author_facet |
Turner, John Hörschgen, Marcus Jung, Wolfgang Turner, Peter |
author_sort |
Turner, John |
title |
SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
title_short |
SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
title_full |
SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
title_fullStr |
SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
title_full_unstemmed |
SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment |
title_sort |
shefex 2 - the vehicle, subsystems and mission concept for a hypersonic re-entry flight experiment |
publishDate |
2007 |
url |
https://elib.dlr.de/81994/ https://elib.dlr.de/81994/1/Visby-Turner-Report-SHEFEX_2.pdf |
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Andøya |
genre_facet |
Andøya |
op_relation |
https://elib.dlr.de/81994/1/Visby-Turner-Report-SHEFEX_2.pdf Turner, John und Hörschgen, Marcus und Jung, Wolfgang und Turner, Peter (2007) SHEFEX 2 - The Vehicle, Subsystems and Mission Concept for a Hypersonic Re-entry Flight Experiment. In: Symposium Proceedings. 18th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2007-06-03 - 2007-06-07, Visby, Schweden. |
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